What was found
DURING INSPECTION OF WING IAW AD 2000-25-02R1, FOUND CRACK IN REAR SPAR ABOUT THREE INCHES LONG. ORIGINATES FROM FLAP SUPPORT BRACKET ATTACH POINT OUTWARD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION OF WING IAW AD 2000-25-02R1, FOUND CRACK IN REAR SPAR ABOUT THREE INCHES LONG. ORIGINATES FROM FLAP SUPPORT BRACKET ATTACH POINT OUTWARD.